Garmin G1000 Airplane Flight Manual Supplement page 29

MOONEY
M20R
loss of any of these inputs. The AHRS will align while the aircraft is in
motion, but will align quicker if the wings are kept level during the align-
ment process.
The Air Data Computer (ADC) provides airspeed, altitude, vertical
speed, and air temperature to the display system. In addition to the pri-
mary displays, this information is used by the FMS and TIS systems.
Engine instruments are displayed on the MFD. Discrete engine sensor
information is processed by the GARMIN Engine Airframe (GEA) sub--
system. When an engine sensor indicates a value outside the normal
operating range, the legend will turn yellow for caution range, and turn
red and flash for warning range.
The G1000 also interfaces to the STEC 55x autopilot and repeats the
autopilot mode annunciators on the G1000 PFD. This provides easy
viewing of the autopilot operating mode and status, but remains a sup-
plemental display of autopilot operating modes.
The GDL 69A is a remote sensor that receives broadcast weather data
from a service of XM Satellite Radio and delivers the data to to the
G--1000 MFD. Highly reliable, near real--time weather information is
transmitted to the aircraft via XM Satellite Radio. XM WX Satellite
Weather service operate in the S--band frequency to provide continu-
ous uplink capabilities at any altitude throughout North America. Also
available with the GDL--69A is XM's digital audio entertainment, which
provides 130--plus channels of music, news, talk, sports and informa-
tion. For detailed operating instructions, see Garmin G--1000 Cockpit
Reference Guide for the Mooney M20R.
The TSO'd KN 63, if installed, is a complete 100 watt, 200--channel re-
mote DME system. Distances up to 389 nm (at line--of--sight altitude),
groundspeeds up to 999 knots and time--to--station up to 99 minutes are
computed digitally and displayed on the G--1000 PFD and controlled by
the G--1000 interface controls. Distance lock--on is virtually instanta-
neous (usually within one second) with accurate groundspeed and
time--to--station readouts following in less than a minute. For detailed
operating instructions, see Garmin G--1000 Cockpit Reference Guide
for the Mooney M20R.
The TSO'd Becker ADF 3502--(2) Automatic Direction Finder system, if
installed, provides accurate bearing--to--station in the 200 kHz to 1799
kHz frequency range, complete with ADF, ANT and BFO tuning modes,
plus audio output for station identification and monitoring AM broad-
casts. It is displayed on the G--1000 PFD and controlled by the PFD in-
terface controls. For detailed operating instructions, see Garmin
ISSUED 11 - 2004
REVISION A 06--2005
REVISION B 03--2006
GARMIN G1000 INTEGRATED AVIONICS SYSTEM
AFM SUPPLEMENT
29 of 33
FAA APPROVED